View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48228U 26145.34681438 +.00000000 +00000-0 -32066-4 0 00004
2 48228 87.8943 294.2607 0002058 99.1911 260.9452 13.14501349 09
| Epoch (UTC): | 25 May 2026 08:19:24 |
| Eccentricity: | 0.0002058 |
| inclination: | 87.8943° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2607° |
| argument of perigee: | 99.1911° |
| revolutions per day: | 13.14501349 |
| mean anomaly at epoch: | 260.9452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|